EP3311448B1

EP3311448B1 - Satellite ground terminal utilizing frequency-selective surface duplexer

Info

Publication number: EP3311448B1
Application number: EP16734113.0A
Authority: EP
Inventors: Thomas Jackson; Peter Hou
Original assignee: Hughes Network Systems LLC
Current assignee: Hughes Network Systems LLC
Priority date: 2015-06-19
Filing date: 2016-06-17
Publication date: 2023-08-02
Anticipated expiration: 2036-06-17
Also published as: EP3311448A1

Description

Technical Field

The disclosed technology relates generally to satellite ground terminals, and more particularly, some embodiments relate to satellite ground terminals utilizing a frequency-selective surface module as a frequency duplexer.

Description of the Related Art

Satellite ground terminals, such as the very small aperture terminal (VSAT), enable duplex communication within a communication network via a single reflector antenna system. The data signal transmitted from the VSAT to the satellite is called the uplink signal, and the data signal received by the VSAT from the satellite is called the downlink signal. Traditionally, the VSAT 100 is feed fed, meaning that a transceiver module 102 with a feed horn antenna located at the focal point of the reflector dish 104 of the VSAT 100 radiates the reflector dish, as illustrated in Figure 1. The reflector dish 104 focuses the downlink signal 106 from the satellite to the feed horn of the transceiver module 102. For the uplink signal 108, the reflector dish transforms a spherical uplink signal radiated by the feed horn antenna of the transceiver module into a planar uplink signal for transmission to the satellite.
A single feed horn antenna is configured to receive and transmit both uplink and downlink signals over a particular band of frequencies, such as K_a band, K_u band, C, or other frequency bands. The design of the feed horn antenna must account for the differences between the uplink communication path and the downlink communication path. A balance must be struck between the gain requirements of the downlink path and the specific envelope standards for the uplink signal dictated by governmental regulations, such as those promulgated by the FCC.
It is necessary to separate the uplink signal from the downlink signal conveyed by the feed horn antenna. In order to separate the two signals, several waveguide devices are attached to the feed horn antenna. Each signal travels at slightly different frequencies within a specific frequency band. For example, some satellite communication occurs over the 30/20 GHz band, with the uplink signal at 30 GHz and the downlink signal at 20 GHz. The waveguide components act to separate the signals and transfer each separate signal to the correct processing circuitry for each communication path. Such separation is necessary to protect the low-power downlink side components from the high-power uplink signal.
The waveguide components are machined from metals, such as copper, aluminum, brass, and zinc, adding extra weight to the system that must be supported by the mast of the VSAT. In addition, it is expensive to machine the different waveguide devices, such as the orthomode transducer, due to the high precision necessary to achieve operational requirements.
US 2003/234745 discloses a dual-band high efficiency hybrid offset reflector antenna system that includes a low frequency antenna including a paraboloidal main offset reflector for reflecting a low frequency signal, as well as a high frequency antenn including both the main offset reflector and a hyperboloidal subreflector for reflecting a high frequency signal discrete from the low frequency signal. The hyperboloidal subreflector includes a frequency selective surface that passes the low frequency signal reflected by the paraboloidal main offset reflector with low subreflector diffraction loss, and that is highly reflective at the high frequency.
EP0689264 describes an antenna with one feed for an S-band electromagnetic signal, and a second feed constructed as an array of radiators to service two C-band signal channels. A subreflector having a microwave frequency selective surface (FSS) is placed in front of a main reflector. The lower frequency S-band feed is located behind and to the side of the subreflector for transmission of radiation via a folded optical path to the main reflector. The C-band feed is located in front of and to the side of the subreflector for transmission of radiation along a straight path through the FSS to the main reflector.
"Dichroic Antenna Reflector for Space Applications", by A. Derneryd et al., Ericsson Review, Telefonaktiebolaget L M Ericsson, SE, (19910101), vol. 68, no. 2, ISSN 0014-0171, pages 22 - 33, XP000233162, discloses a frequency selective surface consisting of a metallic pattern on a carrier made of dielectric material. The frequency selective surface acts as a subreflector, which gives access to both primary and secondary foci. Signals from the feed horns in the secondary focus are reflected, while at the same time, the surface is almost completely transparent to the lower frequencies from the feed horns in the primary focus.
WO02073740 describes a multi-band reflector antenna having a main reflector defining a prime focus and a frequency selective surface sub-reflector defining an image focus. One or more transmitter or receiver feeds are provided at each of the prime focus and image focus. In one application as a ground satellite terminal, the antenna supports ka-band two-way broadband Internet access bundled with multi-satellite Ku-band direct broadcast television service.
JP S54 114065 discloses an antenna system including a main reflector and a primary feed, together with a secondary reflector to guide the wave radiated from the feed toward the main reflector

Brief Summary of Embodiments

According to the present invention, a very small aperture terminal (VSAT) for a satellite communication system is provided, according to Claim 1.
According to various embodiments of the disclosed technology, a system is provided for conducting duplex satellite communication using a single VSAT without the need for expensive and heavy waveguide devices attached to the antenna. A frequency- selective surface module including a frequency-selective surface placed within the optical path between the reflector and the focal point of the reflector acts as a frequency duplexer to separate the uplink from the downlink signal. In addition, by separating the two signals earlier in the optical path, the components of the transmit communication path and the receive communication path may be independently located within the VSAT. This enables optimization of the feed horn antenna and other components connected to each separate communication path, eliminating the need to tradeoff between efficiency and isolation as required when both communication paths are co-located.
Other features and aspects of the disclosed technology will become apparent from the following detailed description, taken in conjunction with the accompanying drawings, which illustrate, by way of example, the features in accordance with embodiments of the disclosed technology.

Brief Description of the Drawings

The technology disclosed herein, in accordance with one or more various embodiments, is described in detail with reference to the following figures. The drawings are provided for purposes of illustration only and merely depict typical or example embodiments of the disclosed technology. These drawings are provided to facilitate the reader's understanding of the disclosed technology and shall not be considered limiting of the breadth, scope, or applicability thereof. It should be noted that for clarity and ease of illustration these drawings are not necessarily made to scale.

FIG. 1 illustrates an example of a traditional satellite communication terminal.
FIG. 2 illustrates an example outdoor unit, and the components thereof, traditionally used in separating the uplink signal and the downlink signal.
FIG. 3 illustrates a satellite ground terminal utilizing a frequency-selective surface module in accordance with one embodiment of the technology herein disclosed.

The figures are not intended to be exhaustive or to limit the invention, which is defined only by the appended claims, to the precise form disclosed.

Detailed Description of the Embodiments

Embodiments of the technology disclosed herein are directed toward a device for duplex satellite communication over a single antenna. More particularly, various embodiments of the technology disclosed herein relate to a satellite ground terminal utilizing a frequency-selective surface module including a frequency-selective surface as a sub-reflector acting as a frequency duplexer to separate the uplink and downlink signals.
As discussed above, it is desirable that the VSAT 100 be able to provide a certain degree of separation between the uplink signal and the downlink signal to avoid an unacceptable level of crosstalk interference and to avoid damage to sensitive receiver components. FIG. 2 illustrates a traditional transceiver module 200 used to separate the uplink and downlink signals in a VSAT, such as the VSAT 100 shown in FIG. 1. Generally, the components of transceiver module 200 is referred to as the outdoor unit (ODU) of the VSAT. A feed horn antenna 202 is positioned at the focal point of a reflector dish and conveys both the uplink signal and the downlink signal over a data signal 204. Attached to the feed horn antenna 202 is an orthomode transducer (OMT) 206. The OMT 206 serves to combine or separate the uplink signal 208 and the downlink signal 210. When implemented in a VSAT, the OMT 206 orthogonally polarizes an uplink signal 208 and downlink signal 210 such that the two signals are at 90° to each other. Orthogonally polarizing the signals allows for greater isolation and decreased interference between the signals. The OMT 206 directs the downlink signal 210 to the downlink signal path.
The uplink signal 208 enters the OMT 206 from a block-up converter (BUC) 212. The BUC 212 converts signals received from a subscriber's indoor unit (IDU) from a lower frequency to a higher frequency. The BUC 212 converts the signal such that it falls within one of the radio spectrum bands identified for satellite communication, such as the K_u band, K_a band, C band, or other radio frequency band.
From the OMT 206, the downlink signal 210 enters a low-noise block (LNB) 216. The LNB 216 combines several different components, such as a low-noise amplifier, local oscillator, and frequency mixer, to convert the downlink signal into a range of intermediate frequencies (IF) for carrying the received signal from the VSAT to the IDU using coaxial cable or other inexpensive connector. In addition to the LNB 216, the downlink path may include additional waveguide elements, such as frequency filter 214.
As discussed above, the traditional ODU components are machined from metals, such as copper, aluminum, brass, and zinc. Each additional component adds weight to the VSAT, which should be taken into consideration in designing the overall VSAT. Machining of the ODU components is also expensive. Precise machining is desired for each waveguide component to meet the operational requirements of the VSAT, based on the material, operating frequencies, and filtering needs.
Further, use of a single feed horn antenna requires design trade-offs between the uplink signal and the downlink signal. For the downlink signal, a higher gain results in greater efficiency in the downlink communication path. For the uplink signal, regulatory rules govern how the uplink signal must operate within the communication band. When using a single feed horn antenna, a trade-off may occasionally be made to sacrifice higher gain to ensure that the uplink signal meets the mandated specifications of the communication band, as outlined by regulatory bodies like the FCC. Separating the components of the two signal paths increases the ability to optimize each signal path individually. Further, such separation also provides complete physical isolation of the two signal paths. This isolation may reduce potential interference between the transmit and receive signals on the different signal paths.
To avoid the need for multiple waveguide devices attached to the VSAT and to allow greater optimization of each communication path independently, a frequency-selective sub-reflector can be used to separate the uplink signal and the downlink signal. FIG. 3 illustrates an example VSAT 300 implementing a frequency-selective surface module in accordance with the present disclosure. The general operation of VSAT 300 is the same as the operation of VSAT 100. VSAT 300 includes a main reflector dish 302, a first feed 304, and a second feed 306. Instead of a single feed horn antenna coupled to both the uplink signal and the downlink signal, the first feed 304 and the second feed 306 each include a separate feed horn antenna. Signal 310 indicates an example signal path between main reflector dish 302 and first feed 304. Likewise, signal 312 indicates a signal path between main reflector dish 302 and second feed 306. In one embodiment, the first feed 304 is connected to the uplink signal path and the second feed 306 is connected to the downlink signal path. In another embodiment, the first feed 304 is connected to the downlink signal path and the second feed 306 is connected to the uplink signal path. In various embodiments, each feed may include a feed horn antenna designed to optimize its respectively assigned uplink signal path or the downlink signal path.
Separation of the uplink and downlink signals is achieved using a frequency-selective surface module 308. The frequency-selective surface module 308 includes a support structure such as, for example, a block of material or a plate, and the support structure includes a frequency-selective surface on at least one face thereof. The frequency-selective surface in some embodiments includes periodic metallic patches designed to be transparent to a range of frequencies, but reflective to others. In operation, the in-band frequencies are capable of passing through the frequency-selective surface, without any effect on the in-band frequencies path of propagation, while the out-band frequencies are reflected off of the frequency-selective surface.
The frequency selective surface is configured to transmit or reflect the RF signals based on their frequency. Accordingly, the frequency-selective surface is configured to act as a filter, such as a pass-band filter. Which frequencies are capable of passing through the frequency-selective surface and which frequencies are reflected depends on the pattern of metallic or dielectric elements embodied on the frequency-selective surface. In other embodiments, the frequency selective surface can comprise a thin surface such as a metallic or dielectric screen or mesh.
As illustrated in the example of FIG. 3, a frequency-selective surface module 308 is mounted so that it is positioned within the signal path between the main reflector dish 302 and the first feed 304 located at or near the focal point of the main reflector dish 302. For example, the first feed 304 may be located before or after the focal point of the main reflector dish, as long as the phase center of the feed horn of the first feed 304 is located at the focal point of the main reflector dish. The frequency-selective surface module 308 is configured to allow signal 310 to pass through the frequency-selective surface module 308 without materially altering the signal path or attenuating the signal 310. Additionally, the frequency-selective surface module 308 is configured such that signal 312 is reflected off of the frequency selective surface to direct signal 312 between main reflector dish 302 and second feed 306.
For example, consider an embodiment in which the antenna is configured such that signal 310 is an uplink signal and signal 312 is a downlink signal. In this embodiment, uplink signal 310 emanates from first feed 304, is allowed to pass through frequency-selective surface module 308 and is reflected off main reflector dish 302 for transmission to the satellite. Also in this embodiment, downlink signal 312 from the satellite is reflected off main reflector dish 302 and subsequently reflected off the frequency-selective surface module 308 and directed toward second feed 306.
As another example, consider an embodiment in which the antenna is configured such that signal 310 is a downlink signal and signal 312 is an uplink signal. In this embodiment, uplink signal 312 emanates from second feed 306 is reflected off the frequency-selective surface module 308 and directed toward main reflector dish 302. Main reflector dish 302 directs the uplink signal 312 toward the satellite. Receive signal 310 is reflected by main reflector dish 302 toward first feed 304. Receive signal 310 is allowed to pass through frequency-selective surface module 308 without material attenuation or alteration of its path.
In various embodiments, the frequency-selective surface module 308 may be constructed using a non-conductive or dielectric base onto which conductive (e.g., metallic) elements are placed. In various embodiments, the conductive elements can be placed in a regular or periodic pattern that is dimensioned to allow one signal at a first frequency (e.g. signal 310) to pass through the frequency-selective surface module 308 without materially attenuating the signal or materially altering the signal path. The patterns can be implemented in various frequency-selective patterns such as, for example, strip gratings having a periodic array of conductive strips; resonant structures such as linear, convoluted and crossed dipoles; mesh or cross-mesh patterns; or other suitable patterns or arrangements. In other embodiments, rather than a patterned surface, three-dimensional structures such as, for example, photonic crystals may be used to provide a frequency selective material.
The conductive patterns can be disposed on a surface of the frequency-selective surface module 308 using any of a number of suitable patterning techniques including, for example, printing or screen printing with conductive inks, patterning conductive paints, photolithography processes, and so on. In various embodiments, the metallic traces may be made of conductive materials such as silver, copper, gold or other conductive elements or alloys. In some embodiments, the non-conductive base may be made using reinforced resins and epoxies (e.g. glass or fiberglass reinforced resins and epoxies such as FR-4), phenolics, plastics, glass, fiberglass and others. In yet another embodiment, selective surface module 308 can be fabricated using a sheet material such as a Mylar or Kapton sheet affixed to a solid surface or mounted in a frame, with the conductive materials patterned thereon. In some embodiments, the non-conductive base may be made of silicon, gallium arsenide, silicon dioxide, sapphire, aluminum oxide, or other non-metallic material suitable for use as the substrate of a printed-circuit board (PCB).
The frequency-selective surface module 308 acts as a sub-reflector for a signal to which the module is not transparent. For example, as illustrated in FIG. 3, the frequency-selective surface module 308 is configured to allow the signal 310 to pass through the module, while signal 312 would reflect off the frequency-selective surface module 308. In this way, the frequency-selective surface module 308 separates the downlink signal 312 from the uplink signal 310 without the need for expensive and heavy waveguide devices. In various embodiments, the frequency-selective surface module 308 may be configured as having a flat surface, while in other embodiments the surface can have a contour such as, for example, a parabolic contoured surface.
The mounting location of the frequency-selective surface module 308 is adjustable, to allow for optimal placement of module 308 within the optical path of the main reflector dish 302. In some embodiments, the frequency-selective surface module 308 may be adjustable in the vertical direction, the horizontal direction, the angle at which it is mounted or some combination thereof. In this way, the frequency-selective surface module 308 is positioned to optimally reflect one signal between main reflector dish 302 and the second feed 306 while still allowing the other signal to pass between the main reflector dish 302 and the first feed 304. In some embodiments, the frequency selective surface module 308 may include a notched support member such that the surface of the frequency-selective surface module 308 may be raised or lowered to ensure that the surface is within the propagation path of the main reflector dish. In some embodiments, the frequency-selective surface module may include a horizontal adjustment support designed to allow the surface of the frequency-selective surface module 308 to be adjusted in the horizontal direction. For example, horizontal adjustment may allow for optimal positioning of the second feed 306 by ensuring that the reflected focus of the frequency-selective surface 308 is at the position of the second feed 306.
Terms and phrases used in the present application, and variations thereof, unless otherwise expressly stated, should be construed as open ended as opposed to limiting. As examples of the foregoing: the term "including" should be read as meaning "including, without limitation" or the like; the term "example" is used to provide exemplary instances of the item in discussion, not an exhaustive or limiting list thereof; the terms "a" or "an" should be read as meaning "at least one," "one or more" or the like; and adjectives such as "conventional," "traditional," "normal," "standard," "known" and terms of similar meaning should not be construed as limiting the item described to a given time period or to an item available as of a given time, but instead should be read to encompass conventional, traditional, normal, or standard technologies that may be available or known now or at any time in the future. Likewise, where this document refers to technologies that would be apparent or known to one of ordinary skill in the art, such technologies encompass those apparent or known to the skilled artisan now or at any time in the future. The use of the term "module" does not imply that the components or functionality described or claimed as part of the module are all configured in a common package. Indeed, any or all of the various components of a module, whether control logic or other components, can be combined in a single package or separately maintained and can further be distributed in multiple groupings or packages or across multiple locations.
Additionally, the various embodiments set forth herein are described in terms of exemplary block diagrams, flow charts and other illustrations. As will become apparent to one of ordinary skill in the art after reading this document, the illustrated embodiments and their various alternatives can be implemented without confinement to the illustrated examples. For example, block diagrams and their accompanying description should not be construed as mandating a particular architecture or configuration. The scope of the present invention is therefore defined only by the appended claims.

Claims

A very small aperture terminal, VSAT, for a satellite communication system, comprising:
a main reflector (302) having a prime focus;

a first feed (304) located at the prime focus of the reflector (302) and in optical communication with the reflector (302);

a frequency-selective surface module (308) having a reflected focus and located at a point along a communication path between the main reflector (302) and the first feed (304), wherein the frequency-selective surface module (308) is configured to be transparent to a first set of frequencies such that a first signal within a first set of frequencies transmitted on a carrier signal passes through the frequency-selective surface module (308); and wherein the frequency-selective surface module (308) is configured to be reflective to a second set of frequencies such that a second signal within a second set of frequencies transmitted on a carrier signal is reflected; and

a second feed (306) located at the reflected focus of the frequency-selective surface module (308) and in optical communication with the frequency-selective surface module (308),

wherein (i) the first feed (304) is configured to transmit uplink signals within the first set of frequencies and the second feed (306) is configured to receive downlink signals within the second set of frequencies or (ii) the first feed (304) is configured to receive downlink signals within the first set of frequencies and the second feed (306) is configured to transmit uplink signals within the second set of frequencies, and

wherein a mounting location of the frequency-selective surface module (308) is adjustable to allow for optimal placement of the frequency-selective surface module (308) within the communication path between the main reflector (302) and the first feed (304).
The VSAT of claim 1, wherein the first feed (304) comprises a transmitter chain module when the first feed (304) is configured to transmit uplink signals and the second feed (306) comprises a receiver chain module when the second feed (306) is configured to receive downlink signals; or
the first feed (304) comprises a receiver chain module when the first feed (304) is configured to receive downlink signals and the second feed (306) comprises a transmitter chain module when the second feed (306) is configured to transmit uplink signals.
The VSAT of claim 1, wherein the frequency-selective surface module (308) further comprises a plurality of metallic traces embodied on a non-metallic parabolic sub-reflector surface.
The VSAT of claim 3, wherein the plurality of metallic traces are arranged in a pattern designed to allow the first signal within the first set of frequencies to pass through the frequency-selective surface module (308).
The VSAT of claim 4, wherein the pattern comprises one or more of: strip gratings having a periodic array of conductive strips, mesh patterns, and cross-mesh patterns.
The VSAT of claim 3, wherein the non-metallic parabolic sub-reflector surface comprises one or more of: resin, epoxy, plastic, phenolics, glass, fiberglass, silicon, gallium arsenide, silicon dioxide, sapphire, and aluminum oxide.
The VSAT of claim 1, wherein the frequency-selective surface module (308) is adjustable in one or more of a horizontal direction, a vertical direction, and an angular direction.
The VSAT of claim 1, wherein each of the first feed and the second feed comprises a respective feed horn antenna.
The VSAT of claim 1, wherein the frequency-selective surface module (308) is adjustable in a horizontal direction to ensure that the second feed (306) is located at the reflected focus of the frequency-selective surface module (308).
The VSAT of claim 9, wherein the frequency-selective surface module (308) has a parabolic shape.
The VSAT of claim 9 or claim 10, wherein the frequency-selective surface module (308) comprises a non-metallic base with a plurality of metallic traces embodied thereon.
The VSAT of claim 11, wherein the plurality of metallic traces are arranged in a pattern designed to allow the first signal within the first set of frequencies to pass through the frequency-selective surface module (308).
The VSAT of claim 12, wherein the pattern comprises one or more of: strip gratings having a periodic array of conductive strips, mesh patterns, and cross-mesh patterns.